Aircraft Configuration
IFR Configured
6800 MTOW Upgraded
AIRFRAME
ROTORS AND CONTROLS
- Fully articulated Main Rotor (M/R) with five composite blades, five
- Elastomeric bearings and five hydraulic dampers
- Rotating M/R flight controls
- Main rotor hub beanie
- Three main dual servo actuators
- Fully articulated Tail Rotor (T/R) with four composite blades, four Elastomeric bearings and four elastomeric dampers
- Rotating TR flight controls
- One TR dual servo actuator
- Force trim system
- Pilot fixed flight controls (cyclic, collective, anti-torquepedals)
- Copilot fixed flight controls (cyclic, collective, anti-torque pedals)
- Dual digital 3-axis linear actuators
- Rotor brake
- Provision for main rotor tracking (magnetic pick-up)
ELECTRICAL SYSTEMS
- DC primary power generation: 28 V DC regulated voltage provided by two independent 300 A starter generators
- DC External Power Receptacle
- Two Nickel-Cadmium Batteries: one 40 Ah main battery plus one 27 AH auxiliary battery
- DC Starter Generator Control Units (2)
- Navigation lights (3)
- Anti-collision light
- External emergency landing lights on the sponsons (2)
- Fixed landing/taxi lights on the sponsons (2)
- Rotating/ retracting landing light
- Baggage compartment lighting (3) and smoke sensor
TRANSMISSION / DRIVE SYSTEM AND HYDRAULIC SYSTEM
- Main transmission with two direct drive engine inputs
- Three main transmission chip detectors/debris collectors with burning capability
- Two free wheel units
- Four strut rods for upper deck attachment and one anti-torque plate
- Intermediate gearbox with sight gauge and magnetic drain plug/chip detector
- Tail gearbox with sight gage and magnetic drain plug/chip detector
- Dual independent, redundant hydraulic systems
- Two hydraulic Power Control Modules (PCMs)
- Three main transmission driven hydraulic mechanical pumps for controls, landing gear and wheel brake actuation
- One electrical pump for control checks on ground (engines off)
- Air conditioning compressor quill
POWER PLANT & FUEL SYSTEM
- Two Pratt & Whitney Canada PT6C-67C engines
- Two independent FADEC systems (one on each engine) with auto start and engine control functions for normal, emergency and training operations
- Two magnetic chip detectors
- Two integrated and independent engine oil coolers
- Separate firewall protection for each engine
- Fire detection system
- Fire extinguisher system (2 bottles)
- Engine exhausts and ejectors
- Two independent crashworthy fuel cells
- Two supply pumps on engines
- Two booster pumps submerged in fuel tanks
- Two fuel filter assemblies
- Two engine back-up controls, mechanical and electrical
- Two manual engine start and ignition systems
STANDARD AVIONICS PACKAGE
- 1st PFD (Pilot Primary Flight Display 8" x 10" color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data
- 2nd PFD (Copilot Primary Flight Display 8" x 10" color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data
- 1st MFD (pilot Multifunction Display 8" x 10" color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data
- 2nd MFD (Copilot Multifunction Display 8" x 10" color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data
- One Electronic Standby Instrument System (ESIS) (attitude, airspeed, altitude, vertical speed, compass, and ILS data)
- Two Attitude and Heading Reference Systems (AHRSs)
- Two Air Data Modules (ADMs)
- Two flux valves
- Two Display Controllers (DCs)
- Two Cursor Control Devices (CCDs)
- One Reversion Control Panel (RCP)
- One Display Dimming Control Panel (DCP)
- One Stability Augmentation System (SAS) control panel
- Two Remote Instrument Controllers (RICs)
- Two Modular Avionic Units (MAUs) incorporating the following major subsystems and/or functions:
- Vehicle Monitoring System - VMS (dual)
- Monitor Warning System - MWS (dual)
- Aural Walling Generator - AWG (single)
- Central Maintenance Computer - CMC (single)
- 4-Axis Digital Automatic Flight Control System - DAFCS (dual) with auto trim function
- Provision for CVR/FDR data interface (single)
- Flight Director System (dual)
- Pilot and copilot microphone and headset
- Pilot and Copilot interphone control (cyclic grip and floor switches)
- Left Modular Radio Cabinet (MRC) with the following modules:
- One VHF Comm
- One Mode-S diversity transponder
- One VORILOC/GSIMB
- One ADF
- One DME
- Two pedestal mounted MCDUs (Multi Control Function Display Units)
- 1st Radar Altimeter (RT - 300)
- 2nd Radar Altimeter System (RT - 300)
- Emergency Locator Transmitter (ELT)
- One Flight Guidance Controller
- Honeywell GPS module with Flight Plan Management System (FPMS)
- Pilot and copilot digital audio panels with remote ICS audio port for ground operation
- Pilot clock (digital)
- Copilot clock (digital)
- One magnetic compass
- One Outside Air Temperature indicator
- Two Master Warning Lights (MWLs)
- Two Master Caution Lights (MCLs)
- Engine 1 Fire Light
- Engine 2 Fire Light
- Baggage compartment smoke detector light
- Dual electrical power connection for CVR/FDR (FAA requirement compliant)
- Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater Locator Beacon (ULB)
INTERIOR TRIM
- Passenger Cabin Interior completion
- Pilot and Co-pilot adjustable seats in lieu of std seats
- Offshore Cabin Basic Settlement, including;
- Silent Soundproofing
- Standard roof liners with dome lights
- Composite liners – Panels
- ICS panel, one position in passengers cabin (LH side)
- P.A. (Passenger Address) system (including loudspeakers) on
- Standard ICS
- Fixed steps for passenger cabin access
- Rubber floor carpet
- 15 seats interior completion
- 15-padded cashworthy comfortable seats fabric or leatherette covered (with inertial reels and safety belts) disposed on 3 rows
- Pilot/ Copilot crashworthy seats (with inertial reels and safety belts)
- Cockpit dome/solid light
- Cockpit utility lights (2)
- 28V DC cockpit/cabin power outlet
- Cockpit panel sun-glare shields
- Overhead cockpit windows sun shades
- Floor provisions for I5-seat configuration
- Fluorescent lighted emergency exit signs
- Cockpit map and data case in central console
- Two flash lights for pilot and co-pilot
- Map and data cases in pilot and co-pilot doors
- ICS Panel with plug for one headset
- Air Ventilation System
- First aid kit
EXTERIOR PAINTING
- Standard polyurethane painting
MISCELLANEOUS
- Covers and flags: engine exhaust pipes (2), engine air inlets (2) and Pitot tubes (2), battery collector warning flag (1)
- Manuals: aircraft log, engines operations, flight and maintenance and overhaul, illustrated parts catalogue
- Tie down-assemblies for main rotor blades (5)
- Tail rotor blades flapping block (1)
- Main rotor blade sock pole (1)
- Main landing gear" wheel chocks (2)
- Main rotor balance and tracking chart, tail rotor balance chart
- Nose landing gear center pin (1) and landing gear handle locking pin (1)
- Jacking dome assembly (1)
- Tow bar (1)
- Loose equipment bag (1)
OPTIONAL EQUIPMENT
